View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 20804U 90083A 23082.90664921 .00000091 00000-0 80717-4 0 9993
2 20804 82.9404 322.5315 0036314 332.4973 37.8077 13.74393460630968
| Epoch (UTC): | 23 March 2023 21:45:34 |
| Eccentricity: | 0.0036314 |
| inclination: | 82.9404° |
| perigee height: | 957 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 322.5315° |
| argument of perigee: | 332.4973° |
| revolutions per day: | 13.74393460 |
| mean anomaly at epoch: | 37.8077° |
| orbit number at epoch: | 63096 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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